A propeller assembly (10) for aircrafts has a hub (12) having at least one receiver opening (16), a receiver (18) located within the receiver opening (16) and having a first collar (20) defining a blade opening (22), a blade (14) having a second collar (24) and a protrusion (26) with the second collar (24) abutting the first collar (20) and the protrusion (26) received within the blade opening (22), and a first retainer (32), and a second retainer (40).
PROPELLER ASSEMBLY AND PROPELLER BLADE RETENTION ASSEMBLY FOR AIRCRAFTS
2015-04-15
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
PROPELLER ASSEMBLY AND PROPELLER BLADE RETENTION ASSEMBLY
European Patent Office | 2018
|Propeller assembly and propeller blade retention assembly
European Patent Office | 2017
|PROPELLER ASSEMBLIES AND PROPELLER BLADE RETENTION ASSEMBLY
European Patent Office | 2016
|Propeller assemblies and propeller blade retention assembly
European Patent Office | 2018
|PROPELLER ASSEMBLIES AND PROPELLER BLADE RETENTION ASSEMBLY
European Patent Office | 2016
|